Question 6 of 7: Psychrometrics and Cooling-Tower Design
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exams — May 2014 — 04-Chem-A3 Mass Transfer Operations. Three-hour, open-book exam; any non-communicating calculator permitted. Format: seven questions in three parts — answer one of Q1–Q2 (Part A), one of Q3–Q4 (Part B) and two of Q5–Q7 (Part C); four questions of equal value constitute a complete paper. All seven are solved below for completeness. Property data (diffusivities, vapour pressures, psychrometric enthalpies) are stated in each Given block; the psychrometric appendix supplied with the exam furnishes the saturated-air data used in Q6.
Reference texts: Geankoplis, Transport Processes and Separation Process Principles (4th ed., Prentice Hall) — molecular diffusion, convective mass transfer, absorption and humidification; Treybal, Mass-Transfer Operations (3rd ed., McGraw-Hill) — gas absorption, wetted-wall and cooling-tower design; Welty, Wicks, Wilson & Rorrer, Fundamentals of Momentum, Heat and Mass Transfer — boundary-layer and falling-sphere correlations; supporting property/psychrometric data from Perry's Chemical Engineers' Handbook (9th ed.).
Question 6: Psychrometrics and Cooling-Tower Design (equal value)
Given. Moist air is cooled below its dew point (dropping liquid water) and then sensibly reheated at constant humidity. Saturation pressures come from the Antoine equation for water and match the supplied psychrometric chart.
Quantity
Value
Initial state
25 °C, 70% RH
Cooled to
15 °C (below dew point ⇒ saturated)
Reheated to
20 °C (constant humidity)
$p_{sat}$: 25/15/20 °C
3.16 / 1.70 / 2.33 kPa
Find. (i) water removed, (ii)–(iii) wet-bulb temperatures, (iv) final RH, (v) final vapour pressure.
Approach. Get the initial humidity from the RH and $p_{sat}(25)$; the air leaves the cooler saturated at 15 °C, so the humidity difference is the condensate; reheating is constant-humidity, fixing the final RH and vapour pressure; wet-bulb temperatures follow from the adiabatic-saturation relation.
(i) Water removed. Cooling to 15 °C saturates the air: $\mathcal H_2 = \mathcal H_{sat}(15) = 0.01060$ kg/kg. Condensate $= \mathcal H_1-\mathcal H_2 = \boxed{0.00327\ \text{kg/kg}\ (3.3\ \text{g/kg})}.$
(iv)–(v) Reheat at constant humidity to 20 °C. $\mathcal H_3=\mathcal H_2$, so $p_{w3} = \dfrac{\mathcal H_3 P}{0.622+\mathcal H_3} = \boxed{1.70\ \text{kPa}}$ and $RH_3 = p_{w3}/p_{sat}(20) = 1.70/2.33 = \boxed{72.9\%}.$
(ii) Initial wet-bulb. Solving the adiabatic-saturation relation $\mathcal H = \mathcal H_{sat}(T_w) - \dfrac{c_s}{\lambda}(T-T_w)$ at (25 °C, $\mathcal H_1$) gives $T_{w,1} = \boxed{21.0\ ^\circ\text{C}}.$
(iii) Final wet-bulb. The same relation at (20 °C, $\mathcal H_3$) gives $T_{w,3} = \boxed{16.8\ ^\circ\text{C}}.$
Quantity
Result
(i) Water removed
3.3 g/kg dry air
(ii) Initial wet-bulb
21.0 °C
(iii) Final wet-bulb
16.8 °C
(iv) Final RH
72.9%
(v) Final vapour pressure
1.70 kPa
Part (b) — Cooling-tower packing height
Given. A counter-current cooling tower analysed by the Merkel enthalpy method; the supplied $k_ca$ (per second) is put on an enthalpy basis with the Lewis-number-one assumption.
Approach. Fix the inlet-air enthalpy from its wet-bulb temperature, set the operating line from the water/air energy balance, integrate the enthalpy transfer units, and multiply by the height of a transfer unit $H_{tOG}=G^{\prime}/(\rho_{air}k_ca)$.
Air-inlet enthalpy. For air–water the wet-bulb is the adiabatic-saturation line, so $H_{G1}=H^*(15\,{}^\circ\text{C})\approx41.9$ kJ/kg.
Operating line. Slope $L^{\prime}c_L/G^{\prime} = (0.556)(4.18)/0.833 = 2.79$ kJ/kg·°C, giving $H_{G2}=41.9+2.79(35-20)=83.7$ kJ/kg at the hot end.
Enthalpy transfer units. $$N_{tOG}=\int_{20}^{35}\frac{(L^{\prime}c_L/G^{\prime})\,dT_L}{H^*(T_L)-H_G(T_L)} = 1.76,$$ evaluated by stepping $T_L$ and reading $H^*(T_L)$ from the saturated-air relation.
Height of a transfer unit (Le = 1). Taking $k_ya\approx\rho_{air}k_ca = (1.185)(2.22)=2.63\ \text{s}^{-1}$-basis, $H_{tOG}=\dfrac{G^{\prime}}{\rho_{air}k_ca}=\dfrac{0.833}{2.63}=0.317$ m.
The gas-phase coefficient supplied as $k_ca$ [s⁻¹] is converted to an enthalpy (mass) basis by assuming a Lewis number of one ($k_ya\approx\rho_{air}k_ca$), the standard air–water approximation. Saturated-air enthalpies use $H^*=(1.005+1.88\mathcal H)T+2501\mathcal H$, which reproduces the supplied psychrometric chart; only enthalpy differences enter $N_{tOG}$, so the datum cancels.